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This report describes the flight test of two Fly-By-Wire flight control systems which use direct drive control valves. The test aircraft is an F-4E and the test systems are used to control the left aileron of the test aircraft. One test system was de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b14370436c7cd0586b485ed8bbaea11
https://doi.org/10.21236/ada117244
https://doi.org/10.21236/ada117244
